A propulsion system with a thrust of 400,000 N is expected to have a maximum thrust misalignment θ of ±0.50? and a horizontal off-set d of the thrust vector of 0.125 in. as shown in the following sketch. One of four small reaction control thrust chambers will be used to counteract the disturbing torque. What should be its maximum thrust level and best orientation? Distance of vernier gimbal to center of mass (CM) is 7 m.
